P92 Eaglet
TECNAM P92-JS · Checklist
Overview
The document is a checklist for the Tecnam P92 Eaglet, an advanced ultra-light aircraft designed for training purposes. It outlines the aircraft's specifications, performance metrics, and key features, emphasizing its suitability for various levels of flight training.
- Designed for Sport Pilot through Commercial training.
- Features a roomy, ergonomic cabin with excellent visibility.
- Equipped with a Rotax 912 ULs2 engine producing 100 hp.
- Maximum takeoff weight is 600 kg (1320 lb).
- Cruise speed at 75% power is 215 km/h (116 kts).
- Stall speed with flaps down is 65 km/h (35 kts).
- Constructed with a monocoque style using aluminum over steel tubing.
- Includes dual flight controls and adjustable seats.
Document
Source
Originally published by tecnamair.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Checklist
- File size ·
- 5.7 MB
- Publisher ·
- tecnamair.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Height m ·
- 2.5
- Length m ·
- 6.5
- Wing span m ·
- 8.7
- Door width m ·
- 0.76
- Wing area m2 ·
- 12.4
- Door height m ·
- 0.83
- Designed mtow kg ·
- 600
- Baggage allowance kg ·
- 20
Performance
- Max speed kmh ·
- 235
- Stall speed kmh ·
- 65
- Cruise speed kmh ·
- 215
- Rate of climb (fpm) ·
- 1200
- Service ceiling m ·
- 4500
- Ground roll landing m ·
- 160
- Ground roll takeoff m ·
- 110
V-speeds
- VNE_KIAS ·
- 270
- VSTALL_KIAS ·
- 65
Weight & balance
- Mtow kg ·
- 600
- Baggage allowance kg ·
- 20
What is the P92 Eaglet?
The P92 Eaglet is a checklist for the TECNAM P92-JS.
Where does the P92 Eaglet come from?
This copy of the P92 Eaglet was originally published by tecnamair.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the TECNAM P92-JS.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More TECNAM P92-JSmanuals & documents
In this document
Specifications
The P92 Eaglet has a maximum takeoff weight of 600 kg (1320 lb) and a baggage allowance of 20 kg (44 lb). Its dimensions include a wingspan of 8.7 m (28.5 ft) and a length of 6.5 m (21.3 ft).
Performance
The aircraft has a maximum speed of 235 km/h (127 kts) at sea level and a service ceiling of 4500 m (14,800 ft). The rate of climb at sea level is 1200 ft/min.
Landing Gear
The main landing gear is made of spring steel, suitable for unimproved strips, and requires no service. The nose gear features a rubber shock absorber system.
Engine and Propeller
Powered by a Rotax 912 ULs2 engine, the aircraft features a fixed pitch wood and composite propeller. The engine is liquid and air-cooled with an integrated reduction gear.
Interior
The cabin is 46 inches wide, featuring adjustable seats, dual control sticks, and ample storage pockets. It is designed for comfort and visibility.
Construction
The aircraft employs a monocoque construction style with aluminum and steel tubing, providing durability and safety.
Safety notes
- Limit loads are +4/-2g and ultimate loads are +6/-3g.
- Ensure proper pre-flight inspections are conducted.
- The aircraft is designed for training environments and should be operated accordingly.
Full document text
P92 Eagletadvanced ultra light P92 EagletTecnam designed the P92 Eaglet after re-examining the ultra light aircraft market and determined a significant need existed for a robust trainer for all levels of flight – Sport Pilot through Commercial training. The result is the Eaglet. Using the proven P92 as the base platform and paying particular attention to the needs of the new American LSA category, Tecnam has delivered the best high wing training and cross country aircraft to date in the light general aviation category. The Eaglet combines the best of the features of their existing high wing aircraft line merged into a single platform. The Eaglet features increased side visibility, smooth aerodynamic lines, a low profile modular panel able to accommodate a wide range of avionics, while still maintaining excellent visibility over the nose, a trait of all TECNAM aircrafts. The doors are fitted with automotive type door seals, seats that give full support with excellent leg room, side map pockets as well as pockets in the back of the seats, and even a cup holder, make the Eaglet a luxury aircraft. All this makes the Eaglet the natural choice for discriminating buyers of all ages and levels of flight experience. But the real beauty of this fine bird is in the flying – uncompromised and unparalleled in feel and response. SpecificationS DeSiGn WeiGHt & LoaDinG kG Lb Designed MTOW 600 1320 Limit Loads +4/-2g Ultimate Loads +6/-3g Baggage Allowance 20 44 DiMenSion M ft WinG Wing Span 8,7 28,5 Wing Area 12,4 M² 133 sqft fuSeLaGe Length 6,5 21,3 Height 2,5 8,2 LH-RH cabin DooR M in Height 0,83 33 Width 0,76 30 enGine Manufacturer Rotax Model 912 ULs2 Power 100 hp Number of Cylinders 4 pRopeLLeR Manufacturer tonini Model gt Number of Blades 2 Type fix peRfoRMance MtoW 450kG/990 Lb SpeeD kM/H ktS Maximum at Sea Level, Gross Weight 235 127 Cruise, 75% power 215 116 VNE 270 146 StaLL SpeeD Flaps Down, power off 65 35 Rate of Climb at Sea Level 1200 ft/M Service Ceiling 4500 14,800 takeoff peRfoRMance M ft Ground roll 110 360 Total over 50 fr obstacle 350 673 LanDinG peRfoRMance Ground roll 160 360 Total over 50 fr obstacle 260 850 fueL Fuel Tank Capacity 45x2 Lt 11,9x2 gaL aDvantaGeS • Superior performance and flight characteristics • Low stall speed with excellent response at all speeds • 116 KTS cruise • Stable and Responsive • Uncompromising build quality: based on CS/VLA certified aircraft P92 JS • Excellent visibility • Roomy, quiet, and ergonomic • Comfortable 46 inch wide cabin advanced ultra light LanDinG GeaR • The main landing gear is spring steel that is robust enough for unimproved strips and requires no service. • The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment. • The main landing gear wheels and brakes are conventional aircraft size (5.00x5) • A hand actuated hydraulic brake is available as an option with toe brakes standard. • A parking brake is between the seats and is actuated by use of a single twist. enGine anD pRopeLLeR • The top and bottom engine cowls are quickly and easily removed making any maintenance procedure faster to accomplish. • The top cowl has 2 large hinged openings for easy access to the engine compartment for effective pre-flight inspections. • The engine is mount is Cro-Moly steel-tubing with shock mounts. • The steel firewall is soundproofed. • The power plant is a Rotax 912 series four-cylinder, four-stroke engine. • The engine is a liquid and air cooled engine with an integrated 1:2.4286 reduction gear. • A fixed pitch wood and composite propeller comes standard with several ground adjustable propellers available as options. • The quick drain gascolator is installed in the engine compartment with easy access. • The engine installation allows for the addition of a 40 Ah external alternator. • Circuit breakers are standard • The battery is located in the rear of the fuselage with easy access through a hinged door. conStRuction • The Tecnam line employs a monocoque construction style using sheet aluminium over steel tubing. • The wing is all aluminium and constructed in a conventional way with a single spar and metal torsion box. • The airfoil is a Gottinga 398 modified for better low speed handling characteristics with a modified STOL wing-tip. • The leading edges of the wings and are easily detachable for repairs. • The fuel tanks hold 11.9 gal in each wing and are located in the wings separated from the fuselage for safety. • A rear window completes the extraordinary visibility allowing 360° of vision in the cockpit. • The stabilator provides remarkable longitudinal hands-off stability along with minimum drag and weight penalty providing balanced, 2 finger, flight control. • The wide slotted flaps, electrically activated, allow stall speed lower than 38 Kts. • The Eaglet has 38 degrees of flaps making steep approach landings easier. inteRioR • Seats are adjustable in flight and increase in height as they are moved forward. • The luggage area allowing for 44 pounds of weight is located behind the seats with ample room for several travel bags • All Tecnam aircraft have dual control sticks with a curve at the base for ease of ingress and egress • The dual controls come standard with PTT and electric stabilator trim on the stick with a trim indicator on the panel. • The widest cabin yet at 46 inches • The interior is spacious, ergonomic and comfortable. • Dual throttles allow the pilot to fly either left or right handed. • Heat and defrost are standard. • The fresh air vents are conveniently located in the doors. • All Tecnam aircraft provide excellent forward visibility over the cowling. • The planes come with dual conventional rudder pedals with a steerable nose wheel. • The wide instrument panel is designed to accommodate a full variety of instrumentation, from a standard 6 pack to fully integrated EFIS installations.
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• The all new instrument panel is modular for ease of avionics installations. advanced ultra light ZaragoZa plant COSTRUZIONI AERONAUTICHE TECNAM S.R.L. Costruzioni Aeronautiche Tecnam operates in three facilities. The Casoria facility is located adjacent to the Napoli Capodichino Airport and covers an area of 10.8000 sq ft with 43.100 sq ft of enclosed facilities. The Capua facility is located adjacent to the “Oreste Salomone” Airport, covers an area of 12.9000 sq ft with 43.100 sq ft of enclosed facilities. Capua has already a new area of 38.7000 sq ft with 64.600 sq ft of enclosed facilities. This extension will double the production capacity of the Capua plant. Modern reinforced concrete buildings are used for manufacturing processes, design activities and office administration. And finally the TECNAM Spain facility located in Villanueva del Gallego, Zaragoza - Spain covers an area of 16.404 sq ft with 65.661 sq ft of enclosed facilities with a runway adjacent of 3.937 length/ft. advanced ultra light VIa MaIorISE 081043 CapUa (CE) ItalY tEl.+39 0823 620134 FaX +39 0823 622899 WWW.tECnaM.CoM InFo@tECnaM.CoM CaSorIa plant CapUa plant StanDaRD equipMent fLiGHt inStRuMentS anD inDicatoRS Magnetic Compass Airspeed Ind., Altimeter Dual Mode (In/Mb) Vertical Speed Bank Indicator Flap Indicator Pitot System Static System Stabilator Trim Position Indicator enGine inStRuMentS Tachometer Hour Recorder Oil Press Oil Temp. Head Temp. Fuel Press. Voltmeter LH + RH Fuel Qty fLiGHt contRoLS Hydraulic Brakes Parking Brake Electrical Flaps Dual Flight Controls Steerable Nose Wheel Stabilator Trim (Electric Actuated From Stick) Engine Controls: Throttle, Two Choke Flight Trim Controls: Stabilator with Indicator Fuel Control Selector with On/Off Panel Switches: Avionic Master eLectRicaL SySteM 12 Volt 18A Amp. Battery 12 Volt Alternators -20 Amp. Switches: Landing Light Strobe Light 12 Volt Socket Circuit Breakers Panel fueL SySteM Two Integral Fuel Tanks with 92 Litres Total Capacity Engine Driven Fuel Pump Fuel Quick Drain inteRioR Pilot and Copilot Seats: Adjustable Fore and Aft Arm Rest Seat Belts & Shoulder Harness, All Seats Wall To Wall Carpeting Map & Storage Pockets Luggage Compartments exteRioR Epoxy Corrosion Proofing, All Structure LH/RH Front Door Pilot/Copilot, Lock and Key Rear Window Main Wheels, 5,00 X 5 Nose Wheel, 4,00 X 6 exteRioR LiGHtS Vertical Tail Strobe Taxi Light cabin confoRt SySteM Windshield Defroster Ventilator Adjustable, 2 Place Heating System with Defrost poWeRpLant anD pRopeLLeR Engines: 1 Rotax 912ULS2 100 Hp, 4 Cylinders Liquid/Air Cooled, Integrated Reduction Gear Dual Ignition System Throttle Control LH/RH Tubular Steel Engine Mount Propeller - Gt Propeller, 2 Blade Fix Propeller Spinner Air Filter Oil Filter Oil and Water Coolers pRoDuct SuppoRt/DocuMentS Manufacturers Full Two Year Limited Warranty Pilots Operation Handbook Maintenance Manual